WO2011159521A2 - Récipients composites résistant à la pression - Google Patents

Récipients composites résistant à la pression Download PDF

Info

Publication number
WO2011159521A2
WO2011159521A2 PCT/US2011/039380 US2011039380W WO2011159521A2 WO 2011159521 A2 WO2011159521 A2 WO 2011159521A2 US 2011039380 W US2011039380 W US 2011039380W WO 2011159521 A2 WO2011159521 A2 WO 2011159521A2
Authority
WO
WIPO (PCT)
Prior art keywords
pressure vessel
resin
pressure
fiber
weight
Prior art date
Application number
PCT/US2011/039380
Other languages
English (en)
Other versions
WO2011159521A3 (fr
Inventor
Kristin L. Thunhorst
Emily S. Goenner
Original Assignee
3M Innovative Properties Company
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 3M Innovative Properties Company filed Critical 3M Innovative Properties Company
Priority to JP2013515379A priority Critical patent/JP6550210B2/ja
Priority to CN201180034874.3A priority patent/CN102985747B/zh
Priority to KR1020137001158A priority patent/KR20130090876A/ko
Priority to EP11796190.4A priority patent/EP2583020B1/fr
Publication of WO2011159521A2 publication Critical patent/WO2011159521A2/fr
Publication of WO2011159521A3 publication Critical patent/WO2011159521A3/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/16—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C1/00—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
    • F17C1/02—Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge involving reinforcing arrangements
    • F17C1/04—Protecting sheathings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0104—Shape cylindrical
    • F17C2201/0109—Shape cylindrical with exteriorly curved end-piece
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0128—Shape spherical or elliptical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/058—Size portable (<30 l)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0604—Liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0607—Coatings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602—Wall structures; Special features thereof
    • F17C2203/0612—Wall structures
    • F17C2203/0614—Single wall
    • F17C2203/0624—Single wall with four or more layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0636—Metals
    • F17C2203/0639—Steels
    • F17C2203/0643—Stainless steels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0636—Metals
    • F17C2203/0646—Aluminium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0636—Metals
    • F17C2203/0648—Alloys or compositions of metals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/0663—Synthetics in form of fibers or filaments
    • F17C2203/0665—Synthetics in form of fibers or filaments radially wound
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/0663—Synthetics in form of fibers or filaments
    • F17C2203/067—Synthetics in form of fibers or filaments helically wound
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0634—Materials for walls or layers thereof
    • F17C2203/0658—Synthetics
    • F17C2203/0663—Synthetics in form of fibers or filaments
    • F17C2203/0673—Polymers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/068—Special properties of materials for vessel walls
    • F17C2203/0697—Special properties of materials for vessel walls comprising nanoparticles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/21—Shaping processes
    • F17C2209/2154—Winding
    • F17C2209/2163—Winding with a mandrel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/221—Welding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2209/00—Vessel construction, in particular methods of manufacturing
    • F17C2209/22—Assembling processes
    • F17C2209/227—Assembling processes by adhesive means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/01—Pure fluids
    • F17C2221/011—Oxygen
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107—Single phase
    • F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/035—High pressure (>10 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/036—Very high pressure (>80 bar)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/05—Improving chemical properties
    • F17C2260/053—Reducing corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/05—Applications for industrial use
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/07—Applications for household use

Definitions

  • the present disclosure relates to pressure vessels, e.g., pipes and tanks, made using fiber composites.
  • the present disclosure relates to pressure vessels formed of fiber composites containing fibers impregnated with a resin system comprising surface-modified nanoparticles dispersed in a matrix resin.
  • pressure vessels are structures capable of containing a fluid, e.g., liquids, liquefied gases, compressed gases, and combinations thereof, under pressure.
  • exemplary pressure vessels include storage containers (e.g., fuel tanks, portable gas (e.g., oxygen) storage bottles, and accumulators) as well as pipes and other conduits that may be used to transport fluids at elevated pressures (e.g., hydraulic lines) and structures exposed to transient elevated pressures (e.g., rocket motor casings and launch tubes).
  • the present disclosure provides a pressure vessel comprising a wall circumferentially enclosing an open volume capable of being filled with a fluid.
  • the wall comprises an interior surface adjacent the open volume and an exterior surface opposite the interior surface, a first end, a second end, and an axial direction.
  • the wall also comprises a composite layer comprising a resin system impregnated with fibers.
  • the resin system comprises a curable matrix resin and a plurality of surface-modified nanoparticles.
  • At least one composite layer comprises fibers aligned at angle of greater than 70 degrees relative to the axial direction. In some embodiments, at least one composite layer comprises fibers aligned at angle of no greater than 40 degrees relative to the axial direction. In some embodiments, at least one composite layer comprises fibers aligned at angle of between 40 and 70 degrees, inclusive, relative to the axial direction
  • the pressure vessel further comprises a first cap, and optionally, a second cap, extending from the wall adjacent the first end and second end, respectively, further enclosing the open volume.
  • a cross section of the wall perpendicular to the axial direction is elliptical. In some embodiments, the pressure vessel is ellipsoidal.
  • the curable matrix resin comprises an epoxy.
  • at least some of the surface-modified nanoparticles comprise a core comprising at least one metal oxide, e.g., silica.
  • a surface- modifying agent covalently is bonded to the surface of the core.
  • at least some of the surface-modified nanoparticles comprise a core comprising calcite.
  • a surface-modifying agent is ionically associated with the core.
  • the resin system further comprises a rubber toughener.
  • the rubber toughener includes a core shell rubber.
  • the wall further comprises a liner having an interior surface adjacent the open space and an exterior surface, wherein the composite layer is adjacent the exterior surface of the liner.
  • the liner comprises at least one a metal and a polymer.
  • the open volume contains a fluid at an absolute pressure of at least 10 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 30 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 40 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 50 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 60 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 70 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 80 MPa. In some embodiments, the open volume contains a fluid at an absolute pressure of at least 90 MPa.
  • FIG. 1 illustrates an exemplary composite pressure vessel according to some embodiments of the present disclosure.
  • FIG. 2 illustrates a cross-section of the composite pressure vessel of FIG. 1.
  • FIG. 3 illustrates a cross-section of another exemplary composite pressure vessel according to some embodiments of the present disclosure.
  • FIG. 4 illustrates an exemplary cylindrical composite pressure vessel according to some embodiments of the present disclosure.
  • FIG. 5 illustrates an exemplary spherical composite pressure vessel according to some embodiments of the present disclosure
  • pressure vessels are classed into four categories based on the materials used for their construction:
  • Type I an all-metal construction (e.g., stainless steel);
  • Type II mostly metal with some fiber overwrap in the hoop direction
  • Type III a metal liner with a full fiber composite overwrap
  • Type IV a polymer liner with a full fiber composite overwrap. In general, as a pressure vessel progresses from Type I to Type IV, the percentage of structural load carried by the fiber composite portion of the structure increases.
  • a fiber composite comprises fibers impregnated with a resin, often called a "matrix resin.”
  • Structural fibers include, for example, glass, aramid, and carbon fibers.
  • Such fibers have stiffness and strength properties that are much higher than the resins used to impregnate them to form the composite.
  • the fibers are in continuous form (that is, not chopped or otherwise discontinuous).
  • the fibers are typically wound around a liner or mandrel such that the length direction of the fibers is aligned in the primary loading directions. This practice takes advantage of the excellent longitudinal stiffness and strength characteristics of structural fibers.
  • the burst strength of the vessel is critical.
  • the walls of a pressure vessel experience a multi-axial load and strain.
  • the hoop load will exceed the axial load.
  • the hoop load will be twice the axial load; thus, the hoop strength will control the burst strength of the pressure vessel.
  • the focus on fiber properties is primarily due to the substantially higher mechanical properties of the fibers relative to the resin.
  • carbon fibers having a tensile modulus of about 200 to about 550 GPa are available.
  • the tensile modulus of a typical matrix resin is one to two orders of magnitude smaller, e.g., the tensile modulus of polyester, epoxies, and cyanate esters is about 3 to 5 GPa.
  • load in the fiber direction i.e., the length direction of the fiber
  • the strength in the fiber direction is dominated by the fiber strength and best use of the high fiber strengths is achieved by orienting the fibers in the primary loading directions of composite pressure vessels.
  • Optimum design of composite pressure vessels requires efficient use of the constituent materials, especially the fiber.
  • the cost, weight, and strength of a pressure vessel are all dominated by fiber utilization.
  • the fiber used is more expensive per weight than the resin constituent, as well as being of higher density.
  • the density of glass fibers is about 2.1 gm/cc, and the density of carbon fibers is about 1.8 gm/cc.
  • the densities of common matrix resins are lower, e.g., about 1.2 gm/cc for vinyl ester and epoxy resins, and about 1.4 gm cc for polyester resins.
  • the density of the fibers is greater than that of the matrix resin.
  • the time, and thus cost, required to fabricate a pressure vessel as well as weight of a design are reduced by reducing the amount of fiber that must be placed during fabrication.
  • Optimum design for a pressure vessel dictates achieving the required strength using the minimum amount of fiber.
  • the tensile modulus of a unidirectional composite can be determined from the rule of mixtures, as shown in Equation 2:
  • ⁇ composite tensile modulus of the fiber composite
  • E ft gj - tensile modulus of the fiber
  • E-resin tensile modulus of the resin
  • Vfiber volume fraction of the fibers relative to the total volume of the fibers and resin.
  • Equation 2 Rearranging Equation 2, and recognizing that the ratio of E res i n over Ej3 ⁇ 4 er is typically less than 0.02 (i.e., 4 GPa for the resin divided by 200 GPa for the fiber), it is clear that, for any practical volume fraction of fibers (e.g., Vf3 ⁇ 4 er > 0.1) the composite modulus is dominated by the fiber modulus.
  • pressure vessel designers could also reduce the weight of a pressure vessel by eliminating composite layers while maintaining the desired strength.
  • FIG. 1 An exemplary pressure vessel is shown in FIG. 1, and a cross-section of this pressure vessel is shown in FIG. 2.
  • Pressure vessel 100 includes wall 110
  • Open volume 120 can be filled with a fluid, e.g., a liquid or gas, under high pressure.
  • Wall 110 comprises interior surface 112
  • Wall 110 also includes first end 116, and second end 118.
  • wall 110 includes fiber composite 130.
  • Fiber composite 130 comprises fibers 133 aligned in the hoop direction, H.
  • the hoop direction is defined relative to the axial direction, A.
  • the hoop direction corresponds to the surface of the pressure vessel defined by a cross-section of the pressure vessel that is perpendicular to axial direction, A.
  • the fibers are impregnated within a resin system that comprises a plurality of surface-modified nanoparticles 144 dispersed in matrix resin 142.
  • the pressure vessel of FIG. 2 is highly simplified compared to commercial pressure vessels.
  • the wall of a pressure vessel includes multiple plies of the same or different fiber composites.
  • the angle of the fibers relative to the axial direction of the pressure vessel can be varied to meet various design considerations.
  • a liner is often used to provide a desired interior wall surface for contact with the fluid and as a form for building up the desired number of composite layers.
  • FIG. 3 illustrates a cross-section of exemplary pressure vessel 200, according to some embodiments of the present disclosure.
  • Wall 210 includes multiple fiber composite layers 230 surrounding open volume 220.
  • Each fiber composite layer 230 comprises fibers impregnated with resin system 240.
  • hoop fibers 233a are substantially aligned in hoop direction, H.
  • the hoop fibers would be aligned precisely in the hoop direction.
  • the fibers are typically spirally wound as continuous tows (i.e., bundles) of fibers. Depending on the number of tows that are simultaneously, spirally wound, the fibers must be aligned at some angle less than 90 degrees relative to the axial direction to minimize overlap between adjacent wraps.
  • the hoop fibers are aligned at an angle greater than 70 degrees relative to the axial direction, in some embodiments, greater than 80 degrees, e.g., greater than 85 degrees, or even greater than 88 degrees, relative to the axial direction.
  • one or more fiber composite layers e.g., fiber composite layer 230b, include axial fibers 233b that are more closely aligned with the axial direction.
  • the axial fibers 233b may be helically wound.
  • the axial fibers are aligned at an angle of no greater than 40 degrees relative to the axial direction, in some embodiments, no greater than 30 degrees, e.g., no greater than 15 degrees, no greater than 10 degrees. In some embodiments, the axial fibers are aligned at an angle relative to the axial direction of between 3 and 15 degrees, inclusive, e.g., between 3 and 10 degrees, inclusive, or even between 5 and 10 degrees, inclusive.
  • one or more fiber composite layers include fibers that are aligned at an angle of between 45 and 70 degrees, inclusive, e.g., between 50 to 60 degrees, inclusive, or even between 53 and 56 degrees relative to the axial direction.
  • an angle of between 45 and 70 degrees, inclusive e.g., between 50 to 60 degrees, inclusive, or even between 53 and 56 degrees relative to the axial direction.
  • a winding angle of 54.7 degrees is used to achieve a 2: 1 ratio of hoop strength to axial strength.
  • the wall comprises liner 270 in addition to the fiber composite layer.
  • the liner is comprised of a metal, e.g. aluminum, steel (e.g., stainless steel), titanium, or combinations thereof.
  • the liner is comprised of polymer, e.g., a polyolefm such as HDPE. Ceramic liners have also been used.
  • the liner itself may comprise multiple layers of the same or different materials. For example, coatings or films may be applied to provide, e.g., erosion resistance, corrosion resistance, and/or chemical resistance and diffusion resistance, including moisture and gas barriers.
  • the interior surface of the liner, or of any optional layer applied to the interior surface of the liner provides the interior surface 212 of wall 210.
  • Coatings or films may also be applied to the composite layers.
  • optional layer 280 is located adjacent the outer surface of the composite layers and provides exterior surface 214 of wall 210.
  • the composition of such an optional layer may be selected to provide any of a variety of desired attributes including, e.g., damage resistance, impact resistance, appearance, smoothness, erosion resistance, corrosion resistance, and/or chemical resistance.
  • Such layers may also be provided as a barrier to constrain the fibers should failure of the composite layers occur.
  • the resin system for at least one fiber composite layer of the pressure vessels of the present disclosure comprises surface-modified nanoparticles dispersed in a matrix resin.
  • the resin system of at least 50%, e.g., at least 80%, e.g., at least 90%), or even all fiber composite layers comprising hoop aligned fibers comprise surface-modified nanoparticles dispersed in a matrix resin.
  • the resin system of at least 50%>, e.g., at least 80%>, e.g., at least 90%>, or even all fiber composite layers (e.g., hoop aligned layers and axial aligned layers) comprise surface- modified nanoparticles dispersed in a matrix resin.
  • pressure vessels may have a wide variety of shapes, they are frequently cylindrical or spherical to maximize volume per unit surface area, and to avoid areas of stress concentration.
  • FIG. 1 a pressure vessel having two open ends was illustrated. As both ends 116 and 118 are open or unsealed, fluid can be pumped through open volume 120, under a pressure constrained by wall 110.
  • a pressure vessel can be selected according to known design considerations.
  • Pressure vessels having a wall with an elliptical, e.g., circular cross-section perpendicular to the axial direction are common.
  • Such pressure vessels may include one or more caps sealing the ends of the elliptical wall.
  • FIGS. 4 and 5 illustrate several other exemplary pressure vessels according to some embodiments of the present disclosure.
  • FIG. 4 shows cylindrical pressure vessel 300, which includes cylindrical wall 310 surrounding open volume 320.
  • Pressure vessel 310 also includes first cap 356 adjacent first end 316 and second cap 358 adjacent second end 318.
  • Caps also called “heads” are used to constrain the fluid within the pressure vessel.
  • the first cap and second cap provide a seal at the ends of wall 310, allowing the resulting enclosed vessel to be pressurized.
  • a cap may be integral to the end of the wall.
  • a cap may be attached, e.g., removably attached, to the end of a wall.
  • the method of attaching e.g., welds, adhesives, and the like, will depend on the materials of construction and other well-understood design parameters.
  • FIG. 4 shows a pressure vessel having a cap on both ends, pressure vessels having a cap on only one end are also possible.
  • Spherical pressure vessel 400 is shown in FIG. 5.
  • spherical wall 410 encloses open spaces 420.
  • a spherical pressure vessel requires the least mass to provide a desired volume and maximum internal pressure.
  • cylindrical pressure vessel 310 and spherical pressure vessel 410 would typically include one or more sealable openings, e.g., valves or threaded fittings, to allow fluid to be introduced into the open space.
  • sealable openings e.g., valves or threaded fittings
  • these same openings, or other openings would be present to allow the discharge of fluid from within the pressure vessel.
  • the fiber composites of the present disclosure comprise fibers impregnated with a resin system.
  • the resin system comprises surface-modified nanoparticles dispersed in a curable resin.
  • any fibers suitable for use in fibrous composites may be used.
  • Exemplary fibers include carbon fibers, glass fibers, ceramic fibers, boron fibers, silicon carbide fibers, polyimide fibers, polyamide fibers, and polyethylene fibers. Combinations of materials may also be used.
  • one or more layers of fiber composite incorporate the fibers as a unidirectional array of individual or bundled continuous fibers, e.g., a tow of fibers.
  • woven fabric, knitted fabric, yarn, roving, braided constructions and non-woven mats of fibers may also be used for some layers.
  • thermosetting resins and radiation-curable (e.g., ultraviolet light-cured or electron beam-cured) resins may be used.
  • Suitable resins include, e.g., epoxy resins, polyester resins, bismalimides resins, cyanate ester resins, vinyl ester resins, acrylic resins, urethane resins, and urethane acrylate resins.
  • polyepoxide resins including aliphatic and aromatic polyepoxide resins, may be used.
  • Exemplary epoxy resins include those based on bisphenol A and bisphenol F, e.g., those available under the trade designation "EPON” from Momentive, Columbus, Ohio (formerly Hexion Specialty Chemicals, Inc., Columbus, Ohio).
  • Other exemplary epoxy resins include low viscosity epoxies, such as those available under the trade designation "HELOXY” from Momentive.
  • the surface modified nanoparticles comprise an inorganic core with one or more surface-modifying agents bonded to the surface of the core.
  • the core comprises a metal oxide. Any known metal oxide may be used.
  • Exemplary metal oxides include silica, titania, alumina, zirconia, vanadia, chromia, antimony oxide, tin oxide, zinc oxide, ceria, and mixtures thereof.
  • the core comprises an oxide of one metal deposited on an oxide of another metal.
  • the core comprises a metal oxide deposited on a non-metal oxide.
  • the core comprises a carbonate, e.g., calcite.
  • Calcite is the crystalline form of calcium carbonate and typically forms rhombohedral crystals.
  • the cores have a primary particle size of between about 5 nanometers to about 500 nanometers, and in some embodiments from about 5 nanometers to about 250 nanometers, and even in some embodiments from about 50 nanometers to about 200 nanometers.
  • the cores have an average diameter of at least about 5 nanometers, in some embodiments, at least about 10 nanometers, at least about 25 nanometers, at least about 50 nanometers, and in some embodiments, at least about 75 nanometers.
  • the cores have an average diameter of no greater than about 500 nanometers, no greater than about 250 nanometers, and in some embodiments no greater than about 150 nanometers.
  • Particle size measurements can be based on, e.g., transmission electron microscopy (TEM).
  • Larger particles or particle aggregates may be filtered or separated from the resin system while the fibers are saturated with the resin system in the process of making a continuous fiber composite. This can result in a non-uniform distribution of particles and resin throughout the final composite resulting in decreased physical properties and the generation of flaw sites for stress concentration.
  • at least 70%, e.g., at least 75% of the nanoparticle cores have an average size of less than 400 nm.
  • the nanoparticles of the present disclosure are surface- modified, i.e., a surface modifying agent is bonded to the surface of the core.
  • the surface-modifying agents of the present disclosure include at least a binding group and a compatiblizing segment: Comp. Seg. - Binding Group;
  • Comp. Seg refers to the compatiblizing segment of the surface-modifying agent.
  • the compatiblizing segment is selected to improve the compatibility of the nanoparticles with the curable resin.
  • the selection of the compatiblizing group depends on a number of factors including the nature of the curable resin, the concentration of the nanoparticles, and the desired degree of compatibility.
  • useful compatiblizing agents include polyalkylene oxides, e.g.,
  • typical compatiblizing agents include satutrated and unsaturated, aromatic or aliphatic hydrocarbons; polyalkane oxides; and combinations thereof.
  • the compatiblizing segment may be selected to provide a positive enthalpy of mixing for the composition containing the surface-modified nanoparticles and the curable resin. If the enthalpy of mixing is positive, the dispersion of nanoparticles in the resin is typically stable. To ensure a positive enthalpy of mixing, the solubility parameter of the compatiblizing segment can be matched to the solubility parameter of the curable resin.
  • the materials can be selected such that the difference in these solubility parameters is no more than 4 cm -J/ anc i [ n some embodiments, no more than 2 J 1/2 cm -3/2 as determined according to Properties of Polymers; Their Correlation with Chemical Structure; Their Numerical Estimation and Prediction from Additive Group Contributions, third edition, edited by D.W. Van
  • the solubility parameter of a material such as a compatiblizing segment or a resin.
  • the solubility parameter of the material can be determined from measurements of the extent of equilibrium swelling of the material in a range of solvents of differing solubility parameters.
  • the solubility parameters of the solvents themselves can be determined from their heats of evaporation.
  • E C oh an d ⁇ can be calculated from the heat of evaporation of the solvent or from the course of the vapor pressure as a function of temperature.
  • a plot of equilibrium swelling of the material versus the solubility parameter of the solvents is generated.
  • the solubility parameter of the material is defined as the point on this plot where maximum swelling is obtained. Swelling will be less for solvents having solubility parameters that are less than or greater than that of the material.
  • the binding group bonds to the surface of the core, connecting the surface- modifying agent to the core.
  • the surface-modifying agents are covalently bonded to the core. This is typical when the core is silica.
  • the surface-modifying agents are ionically bonded to (e.g., associated with) the core. This is typical for calcite cores.
  • Bond energies can be predicted using density functional theory calculations.
  • the calculated bond energies may be at least 0.6, e.g., at least 0.7 electron volts.
  • bond energies of at least 0.8, e.g., at least 0.9, or even at least 0.95 electron volts may be useful.
  • the binding group comprises a phosphonic acid, e.g., surface-functionalizing agents having a formula: Comp. Seg— P— OH
  • the binding group comprises a sulfonic acid, e.g., surface-functionalizing agents having a formula:
  • the surface-modifying agent also comprises a reactive group, i.e., a group capable of reacting with the curable resin, e.g., during the curing process.
  • a reactive group i.e., a group capable of reacting with the curable resin, e.g., during the curing process.
  • the reactive group is selected based on the nature of the curable resin.
  • the reactive group may be located on the end of the compatiblizing segment:
  • Rx. Group is the reactive group.
  • the reactive group may be located along the backbone of or pendant to the backbone of the compatiblizing segment. In some embodiments, the reactive group may be located between the compatiblizing segment and the binding group:
  • a linking group is present connecting the compatiblizing segment with the binding group:
  • compositions of the present disclosure may be cured. In some embodiments,
  • the curable resin is crosslinked. Any known crosslinking method may be used including exposure to thermal energy or actinic radiation (e.g., ultraviolet light and electron beam radiation).
  • the curable resin may also react with the surface-modifying agent.
  • a reactive group of the surface-modifying agent may react with, e.g., covalently bond with, the curable resin.
  • compositions of the present disclosure may include additional additives such as curing agents, cure accelerators, catalysts, crosslinking agents, dyes, pigments, flame retardants, impact modifiers, and flow control agents.
  • the compositions may include tougheners, e.g., rubber tougheners.
  • exemplary rubber tougheners include coreshell rubbers and self-assembling block copolymers.
  • nano-sized coreshell rubber tougheners may be used, i.e., coreshell rubber tougheners having an average size of less than 1 micron. In some embodiments, the nano-sized coreshell rubber tougheners have an average size of less than 500 nm, less than 250 nm, or even less than 100 nm.
  • Exemplary nano-scale coreshell rubber tougheners are available from, e.g., Kaneka Texas Corporation including those available under the trade name "KANE ACE.”
  • phase separating rubbers such as carboxyl-terminated butadiene-acrylonitrile (CTBN) rubber may also be used.
  • micron-sized coreshell rubber tougheners may be used, i.e., coreshell rubber tougheners having an average size of greater than 1 micron, e.g., 1 to 10 microns.
  • Exemplary micron-scale coreshell rubber tougheners are available from, e.g., Rohm & Haas including those available under the trade name "PARALOID.”
  • rubber domains can be created through the addition of self-assembling block copolymers.
  • self-assembling block copolymers are available from, e.g., Arkema, INC., including those available under the trade name "NANOSTRENGTH.”
  • compositions of the present disclosure may be used to form fibrous composites.
  • reinforcing fibers may be impregnated with the composition to form a composite pressure vessel.
  • the resin may then be cured using any known means including exposure to thermal energy and/or actinic radiation.
  • Any known method of producing a pressure vessel may be used. Exemplary methods include wet filament winding in which the fiber tows are impregnated with the resin system prior to their application to liner and dry filament winding in which the fiber tows are first applied to the liner and subsequently impregnated with resin. Braiding may also be used to form the composite pressure vessel. Braiding or winding with "towpreg" is also known for the manufacture of pressure vessels. Towpreg consists of fiber bundles (e.g., tows) pre-impregnated with a resin system. This towpreg can be applied without any additional wet resin, and can be cured directly after application.
  • Towpreg consists of fiber bundles (e.g., tows) pre-impregnated with a resin system. This towpreg can be applied without any additional wet resin, and can be cured directly after application.
  • GC Gas Chromatography
  • TGA Thermogravimetric Analysis
  • the weight of sample (as a percentage of initial weight) remaining at 850 °C was taken as the weight percent of incombustible material and is reported as the weight percent of the product that is silica solids.
  • the residual weight was assumed to be the CaO remaining in the sample after volatilizing all organics and carbon dioxide from the calcite at 900 °C. The calcite weight percent in the original sample was then calculated by dividing the weight percent CaO residue by 0.56.
  • Particle Size Procedure The nanoparticle dispersion was diluted to
  • the optical model for the calculation used a refractive index of 1.6000 for calcite and 1.3591 for the solvent acetone.
  • the second differential method was used for smoothing and was based on 150 iterations.
  • Comparative Example 1 (CE-1). Pressure vessel articles for Comparative Example 1 were made by combining 1.111 parts by weight EPON 828 epoxy resin (obtained from Hexion Specialty Chemicals, Inc., Columbus, Ohio) and 1.00 parts by weight of liquid anhydride curative with promoter, such as that commercially available under the trade designation "LINDRIDE 36Y” from Lindau Chemicals Inc., Columbia, South Carolina, in a plastic container. The two resins were mixed by hand with a wooden stir stick until well mixed (approximately 1-2 minutes). This resin and curative mixture was used to make three individual pressure vessels for CE-1.
  • EPON 828 epoxy resin obtained from Hexion Specialty Chemicals, Inc., Columbus, Ohio
  • liquid anhydride curative with promoter such as that commercially available under the trade designation "LINDRIDE 36Y” from Lindau Chemicals Inc., Columbia, South Carolina
  • Example 1 A fiber composite comprising a resin system containing surface-modified silica nanoparticles was prepared as follows.
  • Surface-modified silica (SMS) nanoparticles were prepared by adding 0.73 parts by weight NALCO 2327 silica (41.1 wt% silica in an aqueous dispersion from Nalco Chemicals, Naperville, Illinois, lot BP9J1622A4) to ajar along with a magnetic stir-bar. The jar was placed on a stir plate and the solution was stirred to create a 2 to 5 cm vortex. Next 1.00 parts by weight methoxy propanol were mixed with 0.03674 parts by weight trimethoxyphenyl silane (Gelest Inc., Morrisville, Pennsylvania, lot number 1B-15944). The resulting
  • methoxypropanol mixture was poured slowly into the jar containing the silica while the mixture was agitated with the magnetic stir-bar. The jar was sealed and placed into a batch oven at 80 °C for 16 hours. The resulting sample, identified as "SMS-1,” contained 16.9 wt% silica.
  • silica nanoparticles were prepared by charging 1.69 parts by weight of silica sol (NALCO 2329K, 40.7 wt% in an aqueous dispersion, lot BP9A1739A0) to an open head stainless steel mixing vessel. Next, 1.00 part by weight methoxy propanol was added slowly while agitating, and then 0.0225 parts by weight of trimethoxy phenyl silane (Gelest Inc., lot 1B-15944) was slowly added to the mixture. The mixture was allowed to agitate with a pneumatically-driven impeller for 30 minutes.
  • silica sol NALCO 2329K, 40.7 wt% in an aqueous dispersion, lot BP9A1739A0
  • a continuous flow hydrothermal reactor such as that described in PCT
  • the 27 liter reactor consisted of 18.3 meters of 1.27 cm outer diameter (OD) (1.09 cm inner diameter (ID)) stainless steel tubing, followed by 12.2 meters of 0.95 cm OD (0.77cm ID) stainless steel tubing, followed by 198.1 meters of 1.27 cm ID polytetrafluoroethylene (PTFE) smooth bore inner tube with a high strength 304 stainless steel braided exterior).
  • OD outer diameter
  • ID inner diameter
  • PTFE polytetrafluoroethylene
  • hydrothermal reactor was maintained at 155 °C, and the backpressure regulator
  • the mixture was metered to the top entrance of a Wiped Film Evaporator (WFE) as described in International Patent Application Number PCT/US 10/35924 ("Process for Making Filled Resins", filed 24- May-2010), i.e., a one square meter WFE counter current polymer processing machine, using a BLB series rotary external spur gear, and a chemical duty gear pump (BUSS FILMTRUDER, Zenith Pumps, Sanford, NC).
  • the WFE rotor (a BUSS Filmtruder-type) was set at a speed of 340 rpm with a 25 Horsepower drive. Vacuum was applied at a level of 2.5 to 2.8 kPa.
  • the feed mixture was subject to the conditions shown in Table 1. After approximately 15 minutes of operation, the product effluent was isolated as a solvent- free, bluish-white, fluid liquid material. Table 1 : WFE process conditions
  • TGA results showed silica solids to be 52.2 wt% in the resin system.
  • Analysis of residual solvent by GC showed less than 0.05 wt% methoxy propanol and no detectable amount of water remaining in the resin system.
  • Example 2 (EX-2).
  • a fiber composite comprising a resin system containing surface-modified calcite nanoparticles was prepared as follows. First, 18,015 grams of calcite (SOCAL 31); 9,608 grams of epoxy resin (EPON 828); 2,402 grams of a diglycidyl ether of cyclohexane dimethanol (HELOXY 107); 1,352 grams of JAS ligand; and 5,500 grams of methyl ethyl ketone (MEK) were premixed with a disperser equipped with an f- blade (BYK-Gardner, Columbia, MD, USA). The JAS was preheated to 90 °C to reduce its viscosity for ease of handling. [0083] The structure of the JAS ligand is:
  • the JAS ligand can be prepared as described of Ligand V in International Patent
  • the two milled batches were then loaded into a 10 gallon stainless steel kettle for stripping of the MEK.
  • the temperature of the batch was increased incrementally over a five -hour period until a nominal batch temperature of 100 °C was reached.
  • An aspirator was used for vacuum and achieved a nominal vacuum of 88 kPa.
  • the vacuum source was switched from the aspirator to a vacuum pump for 15 minutes while maintaining the 100 °C nominal batch temperature.
  • the vacuum pump achieved a nominal vacuum of 91 kPa.
  • the contents of the kettle were then drained.
  • the pressure vessels were prepared by winding carbon fiber (TORAY T700SC- 12000-50C, Lot # A2106M2, Toray Carbon Fibers America, Inc., Decatur, AL) saturated in the epoxy resin system of Example 1, Example 2, or Comparative Example 1 about an aluminum liner (7.5L capacity 6061 T6 Aluminum standard test article liner).
  • the coating process consisted of passing the four tows of fiber across a drum which rotates through a pan of the resin system. The excess resin system was scraped from the drum using a metering blade prior to contacting the fibers. The fibers became saturated with the resin system through the contact with the wet drum and then passed on to the filament winder where they were applied to the aluminum liner.
  • Each vessel was wound with a pattern of 6 hoop layers and 2 helical layers.
  • the winding pattern speeds are listed in Table 2.
  • the hoop speed of Example 2 was reduced relative to the hoop speeds of Example 1 and Comparative Example 1.
  • the temperature of the resin system of Examples 1 and 2 were increased to 27 to 32 °C relative the ambient conditions (i.e., 21 to 24 °C) used for Comparative Example 1. These changes were made to provide the desired resin/curative system transfer to the fibers during the coating process.
  • Table 3 Aluminum liner weight and diameter, and fiber composite cured pressure vessel weight and diameter.
  • the burst pressure was reported as the maximum pressure experienced by the vessel just prior to failure (indicated by a dramatic decrease in pressure).
  • a finite element analysis was performed on the vessels using a non-linear analysis with finite element analysis software, such as "ALGOR FEA" software available from Autodesk, San Rafael, California.
  • the results of the burst test and the calculation of total delivered fiber strength, as well as the coefficient of variation are reported in Table 4.
  • the resin systems containing surface modified nanoparticles provided a dramatic 7% increase in average delivered fiber strength relative to the control sample fiber strength.
  • Table 4 Hydroburst test results.
  • Example 2 were made in an identical manner to those for Comparative Example 1 , except that 5 vessels were prepared, and they were filament wound and cured in two separate batches.
  • Example 3 (EX-3).
  • a fiber composite comprising a resin system containing surface-modified silica nanoparticles was prepared as follows.
  • Surface-modified silica nanoparticles were prepared by charging 1.69 parts by weight of a silica sol (NALCO 2329K, 40.87 wt%> silica in an aqueous dispersion, lot BP0D1847A0) to an open head stainless steel mixing vessel. Next, 1.00 parts by weight methoxy propanol was added slowly while agitating, and then 0.0197 parts by weight of trimethoxy phenyl silane was slowly added to the mixture. The mixture was allowed to agitate with a pneumatically- driven impeller for 30 minutes.
  • hydrothermal reactor was identified as SMS-3.
  • silica nanoparticles were prepared by charging 0.73 parts by silica sol (NALCO 2327, 41.1 wt% silica in an aqueous dispersion, lot BP9J1622A4) to an open head stainless steel mixing vessel. Next, 1.00 parts by weight of methoxy propanol was added slowly while agitating, and then 0.0237 parts by weight of trimethoxy phenyl silane was slowly added to the mixture. The mixture was allowed to agitate with a pneumatically-driven impeller for 30 minutes.
  • silica sol NALCO 2327, 41.1 wt% silica in an aqueous dispersion, lot BP9J1622A4
  • SMS-4 The same continuous flow hydrothermal reactor and reaction conditions described to make SMS-2 was used to prepare SMS-4 except that the TESCOM backpressure gage was maintained at a gage pressure of 2.21 MPa, and the residence time was 35.5 minutes.
  • the effluent from the hydrothermal reactor was identified as SMS-4.
  • a nanoparticle epoxy product was prepared in the same manner as that of EX-1, except the following materials were added to the 380 liter kettle with agitation to form the feed mixture: 5.36 parts by weight SMS-3, 0.88 parts by weight of SMS-4, 1 part by weight methoxy propanol, 1.24 parts by weight epoxy resin (EPON 826), and 0.31 parts by weight a diglycidyl ether of cyclohexane dimethanol (HELOXY 107). This feed mixture was subject to the conditions shown in Table 5.
  • Example 4 (EX-4).
  • a nanoparticle epoxy product was prepared in the same manner as that of EX-1, except the following materials were added to the 380 liter kettle with agitation to form the feed mixture: 5.36 parts by weight SMS-3, 0.88 parts by weight of SMS-4, 1 part by weight methoxy propanol, 1.0 parts by weight epoxy resin (EPON 826), 0.25 parts by weight a diglycidyl ether of cyclohexane dimethanol (HELOXY 107), and 0.30 parts by weight coreshell rubber (KANEKA MX-257).
  • This feed mixture was subject to the conditions shown in Table 5.
  • the temperature of the resin and curative mixture used to make pressure vessels for EX-4 was maintained between 41 °C and 51 °C.
  • the pressure vessels of CE-2, EX-3 and EX-4 were prepared in the same manner with the same equipment, with the same lot of fiber (T700SC), with the same type of aluminum liner, and cured in the same manner as CE-1 and EX-1 and EX-2. The only exceptions are the different resin bath temperatures listed explicitly in EX-3 and EX-4.
  • the winding pattern speeds were not recorded for CE-2, EX-3 and EX-4.
  • the weight and diameter of each aluminum liner was recorded before the filament winding process and again after the winding and curing steps. The results are summarized in Table 6.
  • Table 6 Aluminum liner weight and diameter, and fiber composite cured pressure vessel weight and diameter for CE-2, EX-3 and EX-4.
  • the post-cure weight and diameter of the vessels for EX-3 and EX-4 were greater than the post-cure weight and diameter of the vessels of CE-2. Because all of the vessels of CE-1, CE-2, EX-1, EX-2, EX-3 and EX-4 were made from the same filament winding pattern on the same equipment with the same lot of fiber, they each contained equal weight of carbon fiber.
  • the increase in weight of EX-3 and EX-4 is due to excess resin on the vessel caused by a lack of resin coating and resin bath temperature optimization. Because most of the excess resin was forced to the outside of the vessel during cure (noting a resin-rich appearance on the outside of the cured vessels), the fiber volume of the CE-2 and EX-3 and EX-4 vessels was expected to be
  • control sample fiber strength was calculated by dividing the delivered fiber strength of the article (or average of 2 articles, when applicable) by the delivered fiber strength of the control test vessel (CE-2 vessel #5) after a 365.8 cm impact drop, which showed 2944 MPa (427.0 ksi) and multiplying by 100.
  • the average percentage of virgin fiber strength was calculated by dividing the delivered fiber strength of the article (or average of 2 articles, when applicable) by the average delivered fiber strength of the virgin (no impact) control test vessel (CE-1 vessels #1-3), which showed a delivered fiber strength of 5018 MPa (727.7 ksi) and multiplying by 100.
  • Comparative Example 3 (CE-3). Pressure vessel articles for Comparative Example 3 were made in an identical manner to Comparative Examples 1 and 2, except that 4 vessels were prepared, and they were filament wound with a different composite pattern to provide vessels that were more appropriate for cycle (fatigue) testing.
  • the vessels for CE-1 and CE-2 were intended only for burst testing, not cycle (fatigue) testing.
  • the differences between the vessels of CE-1, CE-2 and those of CE-3 are illustrated by the increase in the post-cure liner diameter and weight (Table 3, Table 6 and Table 8, respectively) and hydroburst pressure, and in the delivered fiber strength from the hydroburst evaluation (Table 9).
  • CE-3 vessels had a composite layer thickness approximately twice as thick as the vessels of CE-1 and CE-2.
  • the delivered fiber strength from the hydroburst test of CE-3 vessel was 4268 MPa (619.1 ksi) whereas that for the CE-1 vessels average fiber delivered strength was approximately 5018 MPa (727.7 ksi).
  • the delivered fiber strength of any particular fiber shows a decrease as the composite layer thickness on the vessel is increased.
  • Example 5 (EX-5).
  • a fiber composite comprising a resin system containing surface-modified silica nanoparticles was prepared as follows. Surface-modified silica nanoparticles were prepared by charging 1.69 parts by weight of silica sol (NALCO 2329K, 40.67 wt% silica in an aqueous dispersion, lot BP0F1998A0) to an open head stainless steel mixing vessel. Next, 1.00 parts by weight methoxy propanol was added slowly while agitating, and then 0.0208 parts by weight of trimethoxy phenyl silane was slowly added to the mixture. The mixture was allowed to agitate with a pneumatically- driven impeller for 30 minutes. [00117] The same continuous flow hydrothermal reactor and reaction conditions described to make SMS-2 was used to prepare SMS-5. The effluent from the silica sol (NALCO 2329K, 40.67 wt% silica in an aqueous dispersion, lot BP0F1998A0)
  • hydrothermal reactor was identified as SMS-5.
  • a nanoparticle epoxy product was prepared in the same manner as that of EX-1, except the following materials were added to the 380 liter kettle with agitation to form the feed mixture: 5.36 parts by weight SMS-5, 0.87 parts by weight of SMS-4, 1 part by weight methoxy propanol, 1.18 parts by weight epoxy resin (EPON 826), and 0.30 parts by weight a diglycidyl ether of cyclohexane dimethanol (HELOXY 107). This feed mixture was subject to the conditions shown in Table 5.
  • Table 8 Aluminum liner weight and diameter, and fiber composite cured pressure vessel weight and diameter for CE-3 and EX-5, vessels prepared for hydroburst and cycle (fatigue) testing. Post-Cure
  • the post-cure weight and diameter of the vessels for EX-5 were greater than the post-cure weight and diameter of the vessels of CE-3. Because the vessels of CE-3 and EX-5 were made from the same filament winding pattern on the same equipment with the same lot of fiber, they each contained equal weight of carbon fiber.
  • the increase in weight of EX-5 is due to excess resin on the vessel caused by a lack of resin coating and resin bath temperature optimization. Because most of the excess resin was forced to the outside of the vessel during cure (noting a resin-rich appearance on the outside of the cured vessels), the fiber volume of the CE-3 and EX-5 vessels was expected to be approximately equal despite the difference in resin weight.
  • Cured Vessel #1 of CE-3 was tested in hydroburst evaluation in the same manner as previously described for CE-1, CE-2, and EX-1 to EX-4, including the rate of pressure increase, but the time required to reach the ultimate burst pressure was greater than that in CE-1, CE-2, EX-1 to EX-4 due to the higher burst pressure of CE-3.
  • Table 9 contains a comparison of the burst pressure for the vessels of CE-3 and CE-1 and the delivered fiber strength calculated by the previously-described finite element model analysis used for CE-1 and EX-1 and EX-2.
  • Cycle Testing The three remaining cylinders of CE-3 and three cylinders of EX-5 intended for cycle (fatigue) testing were subject to autofrettage prior to the cycle tests.
  • the autofrettage consisted of a 58.6 MPa (8500 psi) hold for 2 minutes and hydrostatic test at 37.9 MPa (5500 psi) for 1 minute prior to the commencement of the cycle testing.
  • the cyclic test cycled the vessels between (less than or equal to) 3.1 MPa and 31.0 MPa (4500 psi) using a liquid solution of 25/75 weight ratio of glycol to water at a rate not in excess of 10 cycles per minute.
  • the minimum dwell time in the pressure range between 90 and 100 percent of the upper cyclic pressure was not less than 1.2 seconds.
  • the vessels were cycle tested in parallel using a manifold setup, so they were all exposed to the same cycle testing. The number of cycles to failure (Upper Cyclic Pressure Cycles) was reported for each vessel in addition to the failure location. All the vessels of CE-3 and EX-5 showed failure locations in the vessel sidewalk
  • Table 10 shows a 55% increase in the average cycles to failure of the EX-5 vessels in comparison to the CE-3 vessels. This is a very significant increase in the cycle life of the vessels considering the vessel design was the same, and only the matrix resin was different between CE-3 and EX-5. Higher cycle life enables composite re-design for lower weight and longer-life pressure vessels.
  • the present inventors have discovered that a very significant improvement in composite fiber strength after impact damage could be achieved by incorporating surface- modified nanoparticles, and (in some cases) coreshell nanoparticles in the matrix resin. For example, a 29.6% improvement in delivered fiber strength after impact was achieved by incorporating surface-modified nanoparticles in the matrix resin when compared to a control with no surface-modified nanoparticles. For example, a 40.3% improvement in delivered fiber strength after impact was achieved by incorporating surface-modified nanoparticles and core shell particles in the matrix resin when compared to a control with no surface-modified nanoparticles and no core shell particles. The present inventors have also shown that a very significant improvement in pressure vessel cycle life results from the inclusion of the surface- modified nanoparticles in the matrix resin.
  • the pressure vessels of the present disclosure may be designed to contain fluids have an absolute pressure of at least 2 MPa, e.g., at least 5 MPa, at least 10 MPa, at least 20 MPa, at least 30 MPa, at least 40 MPa, at least 50 MPa, at least 60 MPa, at least 70 MPa, at least 80 MPa, at least 90 MPa, or even greater.
  • the pressure vessels of the present disclosure may be used for any of the wide variety of applications associated with pressure vessels, including, e.g., pipe and conduits, storage containers, and structures exposed to transient elevated pressures.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

La présente invention concerne des récipients résistant à la pression formés à partir de fibres composites. Les fibres composites incluent des fibres imprégnées d'un système de résine contenant des nanoparticules modifiées en surface dispersées dans une matrice de résine durcissable.
PCT/US2011/039380 2010-06-17 2011-06-07 Récipients composites résistant à la pression WO2011159521A2 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2013515379A JP6550210B2 (ja) 2010-06-17 2011-06-07 複合材料圧力容器
CN201180034874.3A CN102985747B (zh) 2010-06-17 2011-06-07 复合材料压力容器
KR1020137001158A KR20130090876A (ko) 2010-06-17 2011-06-07 복합물 압력 용기
EP11796190.4A EP2583020B1 (fr) 2010-06-17 2011-06-07 Récipients composites résistant à la pression

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35576910P 2010-06-17 2010-06-17
US61/355,769 2010-06-17

Publications (2)

Publication Number Publication Date
WO2011159521A2 true WO2011159521A2 (fr) 2011-12-22
WO2011159521A3 WO2011159521A3 (fr) 2012-04-05

Family

ID=45327747

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2011/039380 WO2011159521A2 (fr) 2010-06-17 2011-06-07 Récipients composites résistant à la pression

Country Status (6)

Country Link
US (1) US9822928B2 (fr)
EP (1) EP2583020B1 (fr)
JP (2) JP6550210B2 (fr)
KR (1) KR20130090876A (fr)
CN (1) CN102985747B (fr)
WO (1) WO2011159521A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013053729A (ja) * 2011-09-06 2013-03-21 Nippon Soken Inc 高圧ガスタンク、及び高圧ガスタンクの製造方法
WO2015023718A1 (fr) 2013-08-13 2015-02-19 3M Innovative Properties Company Nanocomposites contenant des nanoparticules de silice pyrogènes sphériques et composites, articles, et leurs procédés de fabrication
EP4215796A1 (fr) * 2022-01-25 2023-07-26 Indian Oil Corporation Limited Récipient sous pression pour stocker un fluide

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2966899B1 (fr) * 2010-10-27 2013-12-20 Air Liquide Procede de fixation d'un equipement sur une paroi et reservoir correspondant
US9004068B2 (en) 2011-05-25 2015-04-14 Scott Technologies, Inc. High pressure air cylinders for use with self-contained breathing apparatus
US9687902B1 (en) * 2011-09-20 2017-06-27 Spencer Composites Corporation Methods for increasing cycle life of metal liners and products manufactured therefrom
WO2014063894A2 (fr) * 2012-10-25 2014-05-01 Siemens Aktiengesellschaft Couche barrière anti-diffusion pour gaines de moteurs
US10309344B2 (en) * 2013-06-07 2019-06-04 Aerojet Rocketdyne, Inc. Stored pressure driven cycle
JP6202978B2 (ja) * 2013-10-17 2017-09-27 日産自動車株式会社 繊維強化複合材料及びそれを用いた圧力容器
JP2017500388A (ja) * 2013-12-13 2017-01-05 ブルー キューブ アイピー エルエルシー コアシェルゴムを含有するエポキシ組成物
JP6348441B2 (ja) * 2014-07-01 2018-06-27 Ｊｘｔｇエネルギー株式会社 複合容器の圧力サイクル試験方法
DE102014016410A1 (de) * 2014-11-05 2016-05-12 Linde Aktiengesellschaft Gasbehälter
US11065827B2 (en) 2015-11-02 2021-07-20 Teijin Carbon America, Inc. Thermoplastic composite in-situ melt processing method for composite overwrapped tools
JP6974334B2 (ja) * 2015-11-02 2021-12-01 テイジン カーボン アメリカ、インコーポレイテッド 複合体オーバーラップツールのための熱可塑性複合体インサイチュー溶融処理方法
EP3225900A1 (fr) * 2016-03-30 2017-10-04 Plastic Omnium Advanced Innovation and Research Récipient sous pression et procédé de formation d'une couche externe d'un récipient sous pression
FR3052228A1 (fr) * 2016-06-01 2017-12-08 L'air Liquide Sa Pour L'etude Et L'exploitation Des Procedes Georges Claude Reservoir composite pour le stockage de gaz sous pression
KR101922103B1 (ko) * 2016-06-13 2019-02-13 회명산업 주식회사 수소저장압력용기 및 그 제작방법
CN105905456B (zh) * 2016-06-20 2018-08-31 北京玻钢院复合材料有限公司 一种纤维增强复合材料双壁储油罐
KR101871283B1 (ko) * 2016-06-28 2018-06-27 현대비에스앤이 주식회사 플라스틱제 압력가스용기
EP3535213B1 (fr) 2016-11-07 2021-06-23 3M Innovative Properties Company Résine durcissable comprenant des nanoparticules comprenant des groupes alkyle à modification hydrophobe liés en surface
KR102043080B1 (ko) * 2017-09-21 2019-11-12 (주)동희산업 고압용기 및 그 제조방법
US10639696B1 (en) * 2017-09-29 2020-05-05 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for outer surface enhancement and compaction of a cylindrical structure using glass failure generated pulse
US10633718B1 (en) * 2017-09-29 2020-04-28 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for inner cylindrical surface enhancement and compaction of a structure using glass failure generated pulse
DE102018121012A1 (de) * 2018-08-28 2020-03-05 Alzchem Trostberg Gmbh Verfahren zur Herstellung eines Druckgasbehälters
CN109707989B (zh) * 2018-11-27 2020-12-25 航天特种材料及工艺技术研究所 一种复合材料球形气瓶及其制备方法
JP2020153503A (ja) * 2019-03-22 2020-09-24 三菱ケミカル株式会社 圧力容器の検査方法
FR3102531B1 (fr) * 2019-10-24 2021-11-12 Ifp Energies Now Réservoir de stockage d’énergie sous forme de gaz sous pression, en béton fibré à ultra haute performance
CN114643481A (zh) * 2020-12-17 2022-06-21 上银科技股份有限公司 回转座及回转工作台
US11841112B2 (en) * 2021-03-24 2023-12-12 Lockheed Martin Corporation Storage vessels with fiber composite reinforcement
CN115091732B (zh) * 2022-08-25 2023-04-11 中材科技（苏州）有限公司 一种复合成型的99MPa级加氢站用储氢容器制法
CN116817176B (zh) * 2023-08-31 2023-11-24 国网浙江省电力有限公司电力科学研究院 一种基于数字孪生的储氢瓶健康状态在线监测方法及***

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5648407A (en) 1995-05-16 1997-07-15 Minnesota Mining And Manufacturing Company Curable resin sols and fiber-reinforced composites derived therefrom

Family Cites Families (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4589562A (en) * 1981-05-04 1986-05-20 Fawley Norman Structures reinforced by a composite material
US4699288A (en) 1986-04-28 1987-10-13 Edo Corporation/Fiber Science Division High pressure vessel construction
JPH06171042A (ja) * 1992-12-07 1994-06-21 Tonen Chem Corp 多層樹脂製燃料タンク
JPH0834554A (ja) 1994-07-22 1996-02-06 Graphtec Corp ロール紙残量検出方法およびその装置
DE59602204D1 (de) * 1995-01-26 1999-07-22 Ciba Geigy Ag Härtbares Epoxidharzgemisch
CN1100665C (zh) * 1995-12-04 2003-02-05 东丽株式会社 压力容器及其制造方法
CA2212244C (fr) 1995-12-04 2007-05-29 Toray Industries, Inc. Recipient de pression et procede pour le fabriquer
JPH1067911A (ja) * 1996-08-28 1998-03-10 Mitsuboshi Belting Ltd 粘着移行性を改善した衝撃・振動吸収性ゲル材
DE19738481C2 (de) * 1997-09-03 1999-08-12 Solvay Alkali Gmbh In Wässrigen Systemen mit oberflächenaktiven Stoffen gecoatetes Calciumcarbonat sowie Verfahren zur gesteuerten bimolekularen Beschichtung von Calciumcarbonat - Teichen
US6074595A (en) * 1998-10-16 2000-06-13 Codeline Corporation Method of making pressure vessels
JP4200250B2 (ja) 1999-10-26 2008-12-24 パナソニック電工株式会社 エポキシ樹脂組成物、プリプレグ、樹脂付き金属箔及び積層板
CH695222A5 (de) * 2001-04-25 2006-01-31 Eva Maria Moser Gasdichter Behälter.
US20030111473A1 (en) * 2001-10-12 2003-06-19 Polymer & Steel Technologies Holding Company, L.L.C. Composite pressure vessel assembly and method
TWI283235B (en) * 2001-11-16 2007-07-01 Maruo Calcium Surface-treated calcium carbonate, production method thereof, and resin composition containing the calcium carbonate
US7803241B2 (en) * 2002-04-12 2010-09-28 Microcosm, Inc. Composite pressure tank and process for its manufacture
US20040052997A1 (en) * 2002-09-17 2004-03-18 Ietsugu Santo Composite pressure container or tubular body and composite intermediate
WO2004031303A1 (fr) * 2002-10-03 2004-04-15 Maruo Calcium Company Limited Carbonate de calcium traite en surface et composition a base de resine contenant ledit carbonate de calcium
JP4354688B2 (ja) * 2002-12-24 2009-10-28 帝人化成株式会社 熱可塑性樹脂組成物
JP2005180605A (ja) * 2003-12-19 2005-07-07 Toyota Motor Corp 貯蔵容器
EP1557442A1 (fr) * 2004-01-23 2005-07-27 SOLVAY (Société Anonyme) Méthode pour le traitement de surface de carbonate de calcium précipité
JP2008500933A (ja) * 2004-05-14 2008-01-17 ソニー ドイチュラント ゲゼルシャフト ミット ベシュレンクテル ハフツング カーボンナノチューブと金属炭酸塩とを具備する複合材料
JP4470578B2 (ja) * 2004-05-17 2010-06-02 日東紡績株式会社 極超低温材料容器用補強材
US7641949B2 (en) * 2004-05-20 2010-01-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Pressure vessel with improved impact resistance and method of making the same
FR2902364B1 (fr) 2006-06-16 2012-04-27 Commissariat Energie Atomique Procede de fabrication d'une vessie d'etancheite en polymere thermodurcissable pour un reservoir contenant un fluide sous pression, tel qu'un reservoir composite, et reservoir
JP2008037951A (ja) * 2006-08-03 2008-02-21 Akebono Brake Ind Co Ltd 摩擦材
KR20090057000A (ko) * 2006-08-29 2009-06-03 쓰리엠 이노베이티브 프로퍼티즈 컴파니 반응성 표면-개질 나노입자를 포함하는 수지 시스템
JP2008101051A (ja) * 2006-10-17 2008-05-01 Konica Minolta Holdings Inc 炭酸塩微粒子の表面処理方法、並びに該微粒子を配合してなる樹脂組成物及びフィルム
GB0622074D0 (en) * 2006-11-06 2006-12-13 Howmedica Osteonics Corp Method of synthesising a nano metic composite and for use thereof in a method for producing a ceramic component
US20080160302A1 (en) * 2006-12-27 2008-07-03 Jawed Asrar Modified fibers for use in the formation of thermoplastic fiber-reinforced composite articles and process
WO2008109011A2 (fr) * 2007-03-02 2008-09-12 Enersea Transport Llc Appareil et procédé permettant l'écoulement de fluides comprimés à l'intérieur et à l'extérieur d'une enceinte de confinement
US7604381B2 (en) * 2007-04-16 2009-10-20 3M Innovative Properties Company Optical article and method of making
JP2008304038A (ja) * 2007-06-11 2008-12-18 Toyota Motor Corp 高圧タンク製造方法、高圧タンク
CN201140876Y (zh) 2008-01-18 2008-10-29 江阴市富仁高科有限公司 钢制强化玻璃纤维制双层油罐
CN102037083B (zh) 2008-03-28 2014-02-05 3M创新有限公司 用于粒子表面改性的方法
JP5676435B2 (ja) * 2008-06-12 2015-02-25 スリーエム イノベイティブ プロパティズ カンパニー ナノ粒子を樹脂と複合する方法
EP2303953A1 (fr) * 2008-07-17 2011-04-06 Dow Global Technologies Inc. Composites de structure dotés d une ténacité améliorée
TWI477528B (zh) 2008-10-07 2015-03-21 Ajinomoto Kk Epoxy resin composition
CN102317361B (zh) 2008-12-19 2014-07-02 3M创新有限公司 纳米方解石复合材料
EP2435178B1 (fr) 2009-05-26 2020-08-12 3M Innovative Properties Company Procédé de fabrication de résines chargées

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5648407A (en) 1995-05-16 1997-07-15 Minnesota Mining And Manufacturing Company Curable resin sols and fiber-reinforced composites derived therefrom

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
COHEN: "The effect of fiber volume fraction on filament wound composite pressure vessels", COMPOSITES: PART B, vol. 32, 2001, pages 413 - 429
EUROPEAN CONFERENCE ON SPACECRAFT STRUCTURES, vol. IN, 12 May 2005 (2005-05-12), pages 1 - 10
See also references of EP2583020A4

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013053729A (ja) * 2011-09-06 2013-03-21 Nippon Soken Inc 高圧ガスタンク、及び高圧ガスタンクの製造方法
WO2015023718A1 (fr) 2013-08-13 2015-02-19 3M Innovative Properties Company Nanocomposites contenant des nanoparticules de silice pyrogènes sphériques et composites, articles, et leurs procédés de fabrication
WO2015069347A2 (fr) 2013-08-13 2015-05-14 3M Innovative Properties Company Nanocomposites contenant des nanoparticules de silice non sphériques; composites, articles et procédés de fabrication correspondants
US10023725B2 (en) 2013-08-13 2018-07-17 3M Innovative Properties Company Nanocomposites containing nonspherical silica nanoparticles, composites, articles, and methods of making same
US10023724B2 (en) 2013-08-13 2018-07-17 3M Innovative Properties Company Nanocomposites containing spherical pyrogenic silica nanoparticles and composites, articles, and methods of making same
US10442914B2 (en) 2013-08-13 2019-10-15 3M Innovative Properties Company Nanocomposites containing silica nanoparticles and dispersant, composites, articles, and methods of making same
US10450444B2 (en) 2013-08-13 2019-10-22 3M Innovative Properties Company Nanocomposites containing spherical pyrogenic silica nanoparticles and composites, articles, and methods of making same
EP4215796A1 (fr) * 2022-01-25 2023-07-26 Indian Oil Corporation Limited Récipient sous pression pour stocker un fluide

Also Published As

Publication number Publication date
EP2583020A2 (fr) 2013-04-24
JP2013530894A (ja) 2013-08-01
EP2583020A4 (fr) 2017-12-27
US20110309074A1 (en) 2011-12-22
CN102985747B (zh) 2015-05-20
JP2019142586A (ja) 2019-08-29
WO2011159521A3 (fr) 2012-04-05
US9822928B2 (en) 2017-11-21
CN102985747A (zh) 2013-03-20
EP2583020B1 (fr) 2021-02-17
JP6550210B2 (ja) 2019-07-24
KR20130090876A (ko) 2013-08-14

Similar Documents

Publication Publication Date Title
EP2583020B1 (fr) Récipients composites résistant à la pression
KR101910202B1 (ko) 분산된 다중모드 표면 개질된 나노입자를 포함하는 수지 시스템
JP2007002256A (ja) プリプレグトウおよび／またはプリプレグの製造方法
JP6039563B2 (ja) ナノ粒子引き抜き成形加工助剤
WO2013015299A1 (fr) Préimprégné et matériau composite renforcé de fibres
WO2007043689A9 (fr) Bouteille de gaz et procédé de production de ladite bouteille de gaz
CN108368281A (zh) 丝束预浸料、复合材料增强压力容器以及复合材料增强压力容器的制造方法
Dell’Anno et al. Effect of water immersion on the interlaminar and flexural performance of low cost liquid resin infused carbon fabric composites
CN115315471A (zh) 预浸料、纤维增强复合材料、高压气体贮藏罐、预浸料的制造方法和高压气体贮藏罐的制造方法
US20140147606A1 (en) Point bridged fiber bundle
CA2823067A1 (fr) Materiau composite
JP2022065282A (ja) トウプレグ、および繊維強化複合材料
JP7463815B2 (ja) プリプレグ、繊維強化複合材、及び高圧ガス貯蔵タンク
JP6581114B2 (ja) 繊維強化樹脂複合体及びその製作方法
WO2022202086A1 (fr) Composition de résine thermodurcissable, préimprégné, matériau composite renforcé par des fibres et récipient de gaz haute pression
JP2013244344A (ja) ゴルフシャフト及びその製造方法
Seferis et al. Cryogenic Cycling Behavior of Polymeric Composite Materials
JP2023025589A (ja) エポキシ樹脂組成物及びその用途
JP2022065281A (ja) トウプレグ、および繊維強化複合材料
Sharma Assessment of small interactions and structural gradient at the interface of FRP composites by FTIR-imaging and DSC techniques
Timmerman Characterization of cryogenic microcracking in carbon fiber/epoxy composite materials
Lee Approve for Public Release: Distribution Unlimited.

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 201180034874.3

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 11796190

Country of ref document: EP

Kind code of ref document: A2

ENP Entry into the national phase

Ref document number: 2013515379

Country of ref document: JP

Kind code of ref document: A

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2011796190

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 20137001158

Country of ref document: KR

Kind code of ref document: A